The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 17, 2020

Filed:

May. 25, 2017
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Helmuth Peter Koelzer, Fort Worth, TX (US);

Brendan Patrick Lanigan, Fort Worth, TX (US);

Michael Kenneth Farrell, Fort Worth, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/14 (2006.01); B64C 29/00 (2006.01); F03D 1/06 (2006.01); B64C 11/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/14 (2013.01); B64C 29/0033 (2013.01); B64C 11/00 (2013.01); F03D 1/06 (2013.01);
Abstract

A proprotor assembly for a tiltrotor aircraft having a forward flight mode. The proprotor assembly includes a spinner subjected to freestream airflow during forward flight. The spinner is elongated to form a tapered leading portion and a substantially cylindrical aft portion. The spinner forms a plurality of rotor blade cutouts exposing an inner chamber. The proprotor assembly includes a plurality of proprotor blade assemblies protruding radially from the spinner through the rotor blade cutouts. The rotor blade cutouts are formed at the substantially cylindrical aft portion of the spinner to reduce the freestream airflow into the inner chamber via the rotor blade cutouts during forward flight, thereby reducing drag experienced by the tiltrotor aircraft.


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